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*»Ht*s>t»t -' •» "^K^" 



ct^/67 

REPORT NO. 6525- V-l 7 



^or^OG 



NEW CAR ASSESSMENT AND STANDARDS 

ENFORCEMENT INDICANT TESTING 

FMVSS NOS, 212, 219 AND 301-75 



Chrysler Corporation 

1979 Chrysler LeBaron 

NHTSA 308-17-458 



CALSPAN C0RP0RATION 
ADVANCED TECHNOLOGY CENTER 
P. 0. B0X 400 
BUFFAL0, NEW YORK 14225 




August 28, 1979 
FINAL REPORT 



Prepared For 

U. S. DEPARTMENT OF TRANSPORTATION 

NATIONAL HIGHWAY TRAFFIC SAFETY ADMINISTRATION 

Enforcement 

Office of Vehicle Safety Compliance 

2100 Second Street, S, W., Transpoint Building 

Washington, D, C. 20590 



This Final Test Report was prepared for the U. S. Department of 
Transportation, National Highway Traffic Safety Administration, 
under Contract No. DOT-HS-8-01938. This document is disseminated 
under the sponsorship of the U. S. Department of Transportation 
in the interest of information exchange. The United States 
Government assumes no liability for its contents or use thereof. 



FINAL REPORT ACCEPTED BY: 



Contract Technical Manager 



Date of Report Acceptance 



n 6525-Y-17 



Calspan 



ASWAMCED T^C33S«©LO<S1f CE&ST!£Sg 



COBPORATIOM P ° BOX 4 °° BUFFALO. NEW YORK 14225 TELEPHONE (716)632-7500 
CaCHe CALSPAN / Tetetyp» 710-523-1863 / Tele* 91-270 



AM A.RVIM COMPAN^ 



TECHNICAL REPORT STAIMDARD TITLE PAGE 



1. Report No. 



2. Government Accession No. 



4. Titie and Subtitle 

NEW CAR ASSESSMENT AND STANDARDS ENFORCEMENT 
INDICANT TESTING - FMVSS NOS. 212, 219 AND 301-75 



7. Author(s) Walter Ef Levanj Test Engineer 

Barbara J, Kelleher, Staff Associate 



3. Recipient's CataJog No. 



5, Report Date 
August 28, 1979 



6. Performing Organi2ation Code 

92325 



8, Performing Organization Report No. 

6525-V-17 



9, Performing Organiiation Name and Address 

Calspan Advanced Technology Center 

P. 0, Box 400 

Buffalo, New York 14225 



10. Work Unit No. 



1. Contracr or Grant No. 
DOT-HS-8-01938 



13. Type of Report and Period Covered 



12. Sponsoring Agency Name and Address 

U, S. Department of Transportation 

National Highway Traffic Safety Administration 

0ffice of Vehicle Safety Compliance 

2100 Second Street» SW. Washington. D. C. 20590 



14. Sponsoring Agenoy Code 

NAD-30 



15. Supplementary 

Reviewed 
Approved 




Project Manager 

Head, Transportation Research Department 
•Calspan Advanced Technology Center 



16. Abstract 

A frontal barrier test of a 1979 Chrysler LeBaron was performed at Calspan 
Corporation, Advanced Technology Center, Transportation Research Department 
facility for the New Car Assessment and Standards Enforcement Indicant Testing of 
FMVSS 212 - Windshield Mounting; FMVSS 219 - Windshield 2one Intrusion; FMVSS No. 
301 - Fuel System Integrity for the Office of Vehicie Safety Compliance, 
the 0ffice of Automotive Ratings and for Research and Development. 

The impact speed was 35.04 mph. 
The post-test vehicle crush was 24.6 inches. 
Intrusion of firewall into compartment was 9.0 inches. 
Test vehicle coraplied in all respects with following: 

1. FMVSS 212 - Windshield Retention, 

2. FMVSS 219 - Windshield Intrusion, 

3. FMVSS 301-75 - Fuel System Integrity, 

FMVSS 208 head injury criteria were exceeded by all of the dummy occupants. 



17. Key Words 



18. pistribution Statement 

Copies of this report are ayailabl e f rom ; 



Technical Reference Division 

National Highway Traffic Safety Admin. 

Room 5108, Nassif Building 

400 7th Street, SW, Washington, D.C. 20590 



19. Security Classif. (of this report) 

Unclassified 



20. Security Classif. (of this page) 

Unclassified 



21. No. of Pages 



22. Price 



Form DOT F 1700.7 (8-69) 



lll 



6525-V-17 



TABLE QF CONTENTS 

Section Pa3e_M 

1 PURPOSE AND TEST PROCEDURE 1-1 

2 SUMMARY 0F TEST NUMBER 17 2-1 

3 SUMMARY OF RESULTS OF FMVSS NOS. 212, 219 3-1 
AND 301-75 

APPENDIX A - PHOTOGRAPHS A-l 

APPENDIX B - VEHICLE AND DUMMY RESPONSE DATA B-1 

APPENDIX C - DUMMY CERTIFICATION TESTS C-l 



IV 652S-V-17 



AN AFU/ir>i COtwl PANV 



PO BOX 400 BUFFALO. NEW YORK 14225 TELEPHONE (716)632-7500 
Cabte: CALSPAN i Teletype 710-523-1363 / Telex 91-270 



LIST 0F FIGURES 



Figure No. 

1 PRE-TEST AND POST-TEST MEASUREMENT POINTS 

2 OCCUPANT CLEARANCE OIMENSIONS 

3 CAMERA POSITIONS FOR FRONTAL/0BLIQUE IMPACTS 

4 VEHICLE ACCELEROMETER LOCATIONS 

5 WINDSHIELD ZONE INTRUSION, FMVSS 219 DATA SHEET 

6 PROTECTED ZONE 

7 SUMMARY OF FMVSS 212 DATA 



Page No. 


2-6 


2-8 


2-9 


2-11 


3-5 


3-6 


3-7 



APPENDIX A 

A-l PRE- AND POST-TEST FRONT VIEWS 

A-2 PRE- AND POST-TEST REAR VIEWS 

A-3 PRE- AND POST-TEST SIDE VIEWS 

A-4 PRE- AND POST-TEST THREE-QUARTER VIEWS 

A-5 PRE- AND POST-TEST UNDERBODY VIEWS 

A-6 POST-TEST UNDERBODY DEFORMATION 

A-7 FUEL CAP 

A-8 POST-IMPACT WINDSHIELD 

A-9 ENGINE COMPARTMENT ACCELEROMETER 

A-10 VELOCITY TRAP COUNTER DISPLAY 

A-ll PRE-TEST OCCUPANT POSITIONS 

A-12 POST-TEST OCCUPANT POSITIONS 



A-2 
A-2 
A-3 
A-4 
A-5 
A-6 
A-7 
A-7 
A-7 
A-7 
A-8 
A-9 



APPENDIX C 
C-l 
C-2 
C-3 
C-4 
C-5 
C-6 
C-7 
C-8 



Calspan 



AM ARVIM COW PAMV 



LUMBAR SPINE FLEXI0N TEST APPARATUS 

ABDOMEN PRESS TEST 

HEAD DROP TEST APPARATUS 

KNEE IMPACT TEST APPARATUS 

THORAX IMPACT TEST APPARATUS 

NECK IMPACT TEST APPARATUS 

PART 572 TEST DUMMY - FRONT AND SIDE VIEW 

ELECTRONIC TEST EQUIPMENT 



PO BOX 400 BUFPALO. NEW YORK 14225 TELEPHOMG (716)632-7500 
CaDle CALSPAN / Teletype 710-523-1663/ Telex : 91-270 



C- 


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-13 


c- 


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c- 


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c- 


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•15 


c- 


-16 


6525- 


-V-17 



LIST 0F TA8LES 

Table No. Pa 9 e No 

1 CRASH TEST SUMMARY 2-2 

2 VEHICLE TEST WEIGHTS AS TESTED 2-4 

3 DUMMY INJURY CRITERIA VALUES 2-5 

4 VEHICLE MEASUREMENTS 2-7 

5 HIGH SPEED CAMERA INF0RMATI0N 2-10 

6 SUMMARY 0F TEST CONDITIONS 3-2 

7 POST IMPACT DATA FOR STANDARDS 219 AND 301 3-4 

8 "FUEL SYSTEM INTEGRITY" POST-IMPACT TEST DATA, 3-8 
FMVSS No. 301-75 



v1 ' 6525-V-17 

CCllSpCin m&wM&meEn technology ce»7 ss? 



AM A.PVIM COMPANY 



PO BOX 400 BUFFALO. NEW YORK 14225 TELEPHONE (716)632-7500 
Cabte: CALSPAN / Tetetype; 710-523-1863/ Telex: 91-270 



SECTION L 
PURPOSE AND TEST PROCEDURE 



PURPOSE: The purpose of this test was to determine whether the subj ect 
vehicle (a 1979 Chrysler LeBaron) meets the requirements of 
FMVSS Nos. 212, 219 and 301-75 at a higher test speed and also 
to obtain structural information and dummy injury criteria values for 
Research and Development and the Office of Automotive Ratings of 
the NHTSA. This test is part of the New Car Assessment Program B.O.A 
Task 2, sponsored by the National Highway Traffic Safety 
Administration (NHTSA) under Contract DOT-HS-8-01938. 



TEST PROCEDURE 



The Calspan Corporation, Advanced Technology Center, 
Transportation Research Department Test Procedure for the 
New Car Assessment Crash Tests submitted to, and approved 
by, the Contract Technical Manager (CTM) contains the specific 
procedures used to perform this test. 

With the exception of a higher test speed, this procedure is 
not in conflict with any portion of FMVSS Procedures issued 
by the Office of Standard Enforcement and the amendments in 
effect as noted by the applicable contract. 



1-1 



652S-Y-17 



SUMMARY 0F TEST NUMBER 17 



A frontal barrier crash test was conducted on a 1979 Chrysler LeBaron 
2-door sedan at an impact velocity o£ 35.04 mph. Photographs of the vehicle 
and occupants can be viewed in Appendix A and Table 1 presents pertinent crash 
test information. 

The vehicle occupants included a 50th percentile Part 572 driver 
wearing a production 3-point belt, a 50th percentile Part 572 right front 
passenger also restrained with a 3-point belt and a lap belted Alderson VIP-6C 
6-year old size ATD center rear seat passenger. The 50th percentile ATD 
certification information is found in Appendix C. Table 3 presents the 
FMVSS-208 injury criteria generated by these occupants and the associated 
data traces, along with vehicle data traces, are provided in Appendix B. 

The maximum vehicle crush of 24.6 inches was measured along the 
vehicle centerline. The maximum intrusion into the occupant compartment was 
9 inches. 

Post-test observations are summarized in General Comments, page 2-3. 



2-1 6525-V-17 



Table 1 



CRASH TEST SUMMARY 



TEST NO. 308-17-458 



DATE: 



8/28/79 



PROJECT: NEW CAR ASSESSMENT PROGRAM 



TIME: 1530 



TEMP: 80° F 



VEHICLE 

TEST WEIGHT (lbs) 

IMPACT ANGLE (deg)* 

IMPACT VELOCITY (mph)** 

MAX. CRUSH (in) 

MAX. INTRUSION (in) 



1979 Chrysler LeBaron 2-Door 



4160 




0° 


35.04 


24.6 


inches 


9.0 


inches 



DUMMIES 

TYPE HYBRID II, PART 572 HYBRID II, PART 572 
LOCATION LFCD RFC2) 

RESTRAINT Production 3-Point Production 3-Point 

System 

NUMBER 0F DATA CHANNELS 
NUMBER 0F HIGH SPEED CAMERAS 



System 



42 



9+1 Real Time 



ALDERSON VIP-6C 
(6 YEAR OLD SI2E) 

CENTER REAR(6) 
Lap Belt 



*With respect to tow track Centerline 
**Speed trap measurement (+ .05% accuracy) 



2-2 



6525-V-17 



GENERAL COMMENTS 



The 1979 Chrysler LeBaron involved in a frontal barrier crash at a 
nominal velocity of 35 mph complied with FMVSS Nos. 212, Windshield Mounting, 
219, Windshield Zone Intrusion and 301-75, Fuel System Integrity. There was 
100% retention of the windshield, no intrusion into the protected zone and no 
fuel leakage. No cracks were observed in the windshield after impact 
(Figure A-8) . 

All of the ATD occupants failed to comply with the FMVSS-208 Head 
Injury Criteria (HIC) limit of 1000. Both the driver and right front 
passenger occupants submarined, their lap belts roped and overrode the pelvic 
regions becoming imbedded in the abdominal regions. The knees of both ATDs 
contacted and slightly deformed the lower instrument panel. The driver con- 
tacted the top rim and the hub of the steering wheel with his head, deforming 
the hub of the steering wheel and forcing the steering column downward. 
There was no apparent head contact between the right front passenger and the 
interior of the vehicle. The head of the 6-year old size ATD in the center 
rear position hit the arm rest between the front bucket seats. The lap belt 
showed no indication of roping. 

Underbody damage can be viewed in Figures A-5 and A-6. The drive 
shaft broke off the differential. A small dent in the fuel tank was caused 
by the end of the rail at the edge of the camera pit and is incidental to 
the vehicle performance. 

Other post-test observations include: 

• Neither door could be opened. 

• Both front tires were pinched but remained inflated. 

• The second velocity trap counter failed to trigger 
(Figure A-10). 



2-3 6525-Y-17 



Table 2 
VEHICLE TEST WEIGHTS ASTESTED 



Left Front noo Ibs 
Right Front 1100 Ibs 
TOTAL FRONT 2200 Ibs 



Left Rear 
Right Front 
TOTAL REAR 



990 Ibs 

970 Ibs 

1960 Ibs 



Total Weight * 2200 + 1960 = 4160 



Ibs 



Wheel Base 
Cg F.W. = 



113 



inches 



1960 ibs x 113 inches 

4160 ] bs 



53.24 



inches 



CALCULATION FOR TEST WEIGHT 



RCLW = Rated Cargo and Luggage Weight 

UDW = Unloaded Delivered Weight ( 3600 Ibs) 

VCW = Vehicle Capacity Weight ( yioo Ibs) 

DSC = Designated Seating Capacity (_6_) 



RCLW = VCW - 150 (DSC) 

RCLW = 1100 - 1 50 ( 6 ) = 

TEST WEIGHT = UDW + RCLW + (No 
TEST WEIGHT = 3600 lbs + _ 
TEST WEIGHT = 4176 1 bs 



200 Ibs 



Dummies X 164 lbs) + CWt. of 6-Yr-Old Size Dummy) 
200 Ibs + 2 (164 Ibs) + 48 lbs> 






2-4 



6525-Y-17 



I ULS t SS *-» 



DUMMY INJURY CRITERIA VALUES 





MAXIMUM ACCELERATION <"G"J * 


HEAD 


CHEST 


PELVIS 


X 


Y 


Z 


R 


X 


Y 


Z 


R 


X 


Y 


Z 


R 


DUMMYIU 


-220 


-60 


95 


235 


-44 


14 


-21 


45 










DUMMY (2) 


85 


9 


69 


102 


-38 


8 


10 


39 










DUMMY (3) 


-79 


-30 


120 


129 


-36 


-11 


51 


59 










OUMMY (4} 





























MAXIMUM FORCE-FEMUR LOAD (LBS) 


RIGHT FEMUR 


LEFTFEMUR 


DUMMY(1) 


300 


740 


DUMMY (2) 


440 


420 


DUMMY (3) 






DUMMY (4) 









MAXIMUM FORCESEAT BELTS LOADS (LBS) 


SHOULDER STRAP 
UPPER BELTLOAO 


LAP STRAP 

BELT L0AD 




DUMMYI1) 


1470 


1270 




DUMMY (2) 


1900 


1490 




DUMMY (3) 








DUMMY (4) 











HEAD INJURY CRITERIA** 


SEVERITY INDEX 


HIC 


t-, (SECJ 


t 2 (SECJ 


AVE. ACC. (g) 
t-, TO t 2 


HEAD 


CHEST 


DUMMYU) 


2402.4 


.0801 


.0888 


150,1 


3395.7 




DUMMY(2) 


1070.8 


.0567 


.1866 


36.8 


1506.5 




DUMMY (3) 


2810.1 


.0858 


.1236 


88.8 


3347.4 




DUMMY (4) 















•DEPINED AS EXCE£D1NG 0.003 SEC. DURATION 
*AS DEPINED IN FMVSS NO. 208 



2-5 



6525-Y-17 



REAR DATUM REFERENCE 



Length of 
Engine Block 



To Trailing Edge 
Behind Door 
(Right/Left Side) 




V\\j in Front of Door 
(Right/Left Side) 



Ctr. of 

Str. 

Coluinn 



XI 7 
To 'A' Post 



X16 

To Strg. Column 



_, REAR DATUM REFERENCS 

^io 8ottom of AT CENTER 0F R£AR 

£- lHn ^ .-, * BUMPER 
(Right/Left side) 

To Firewall (Right/Left Side) 



Figure 1 PRE-TEST AND POST-TEST MEASUREMENT POINTS 

2-6 6525-Y-17 



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2-7 



6525-Y-17 



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Figure 2 OCCUPANT CLEARANCE DIMENSIONS 



2-8 



6525-Y-17 



Note: Camera information shown in Table 5. 



Windshield 

Styrofoam 

Template 



Fixed Collision Barrier 



Camera 7 



i 



Camera mounted 
on top front 
edge of barrier 

T 



Camera 5 




Real Time 
Camera 10 



£ — Concrete Test Pad 



Level ,r tow road 



TOP VIEW 



Figure 3 CAMERA POSITIONS F0R FR0NTAL IMPACTS 



2-9 



6525-V-17 



1 



CAMERA NO 

1 
2 
3 
4 
5 
6 
7 
8 
9 
10 



Table 5 

HIGH SPEED CAMERA INFORMATION 
(Test 308-17-458 ) 
Chrysler LeBaron Frontal 



LOCATION 



SOUTH WIDE 
SOUTH WINDSHIELD 
SOUTH DUMMY 
NORTH DUMMY 
NORTH WIDE 
REAR DUMMY 
BARRIER FACE 
PIT FRONT 
PIT REAR 
SOUTH WIDE 



TYPE 



HYCAM 

FASTEX 

FASTEX 

FASTEX 

FASTEX 

FASTEX 

PHOTOSONICS 

PHOTOSONICS 

PHOTOSONICS 

REAL TIME 



LENS 
(mm) 



25 mm 
50 mm 
50 mm 
50 mm 
35 mm 
50 mm 
8 mm 
13 mm 
13 mm 



SPEED 
(fps) 



1500 
No Pulse 
1000 
1300 
1400 
1350 
1000 
600 
300 
24 



NOTE: (24 fps) real time movie film coverage of pre-crash, post 
crash and crash event spliced at start and end of film. 



2-10 



6525-V-17 




ACCELEROMETER 
NUMBER * 


ACCELEROMETER LOCATION 


DIRECTION 


X 


v 


z 


1 


Engine 


X 




X 


2 


Firewal1 above Steering Colurrin 


X 




X 


3 


Firewall at Vehic1e Centerline 


X 




X 


4 


Front Seat "Crossbeam" 


X 






5 


Rear Seat "Crossbeam" 


X 




X 


6 


CG 


X 


X 


X 



The accelerometer pack number can be correlated with the vehicle 
response data traces found in Appendix B. 



Figure 4 VEHICLE ACCELEROMETER LOCATIONS 



2-11 



6525-V-17 



SECTION 3 
SUMMARY OF RESULTS OF FMVSS NOS, 212, 219 AND 301-75 



Summary of Test Conditions 

Post-Impact Data 

Windshield Zone Intrusion, FMVSS 219 

Protected Zone 

Summary of FMVSS Data 

Fuel System Integrity Post-Impact 



3-1 6525-V-17 



Table 6 
SUMMARY 0F TEST CONDITIONS 



TEST VEHICLE INFORMATION 



Vehicle Manufacturer Chrysler Corporation 
Make/Model LeBaron 



Body Style 2-Door Model Year 1979 

VIN FH22G9G217130 Build Date 4/79 

NHTSA No. 308-17-458 Color Red and White 

Engine Data: 8 cylinders 518 in^/ displacement 

Transmission Data: 3 speed ( ) Manual (x ) Automatic 

Date Vehic1e Received by Laboratory 7/26/79 

Dea1er's Name & Address JKJ Chrvsler 5990 Duke. Alexandria, Va. 

DATA FR0M CERTIFICATION LABEL ON LEFT DOOR REAR FACE OR '3' POST 

Vehicle Manufactured by Chrysler Corporation 



Date of Manufacture 4/79 VIN fh22G9G217150 

GVRW 5Q2S Ibs GAWR: Front 2575 Ibs Rear 25Q0 Ibs 

DATA FROM "RECOMMENDED TIRE PRESSURE" LABEL ON DOOR, POST, GLQVE BOX, ETC. 

Vehic1e Load (up to capacity) - Front 28 psi 

Rear ?a psi 

Recommended Tire Size FR78-15 Load Range: _*_ B C D 

Vehicle Capacity: Types of Seats _X_ Bench Bucket Split Bench 

Number of Occupants (Designated Seating Capacity): 3 Front 

3 Rear 

6 TOTAL 

Cargo Load = 200 1 bs 

TOTAL = lioo 1 bs 

WEIGHT QF TEST VEHICLE AS RECEIVED FROM DEALER (WITH MAXIMUM FLUIDS) 
Right Front = 1040 Ibs Right Rear = 750 Ibs 
Left Front = man Ibs Left Rear = 77 ° Ibs 
TOTAL FRONT WEIGHT = 2 nan Ibs ( ^7.8 % of Total Vehic1e Weight) 
TOTAL REAR WEIGHT = 152Q Ibs ( 42 - 2 % of Total Vehicle Weight) 
TOTAL DELV. WEIGHT = 3600 Tbs 

WEIGHT QF TEST VEHICLE WITH REQUIRED DUMMIES AND 184 Ibs CARGO 

Right Front = hqq Ibs Right Rear = 990 Ibs 

Left Front = 1100 Ibs Left Rear = 970 Ibs 

TOTAL FRONT WEIGHT = 2200 1 bs ( 52.9 % of Total Vehide Weight) 

TOTAL REAR WEIGHT = 1960 Ibs ( 47.1 % f Total Vehicle Weight) 
TOTAL TEST WEIGHT = 4160 Ibs 
Weight of ballast secured in vehicle trunk area = 000 Ibs 

3-2 6525-Y-17 



Table 6 
SUMMARY QF TEST CONDITIONS (Cont'd) 

TEST CONDITIONS 

Date of Test 8/28/79 __ Time of Test 1530 HRS 

Ambient Temperature 80 °F at impact area 

Temperature in Occupant Compartment 8Q °F 
Windshield Molding Temperature 84 °F 

VEHICLE ATTITUDE (all dimensions in inches) 

De livered Attitude: RF 29" LF 28-l/2' T rr 28-3/4" LR 28-1/2" 
Test Attitude: RF 28-3/4" L F 28-1/2" RR 26-3/4" LR 26-1/2" 

VEHICLE TIRE DATA 

Recommended Cold Tire Pressure: Front = 28 psi Rear = 28 psi 

Recommended Tire Size FR78-15 Load Range b 

Tires on Vehicle FR78-15 General 

Is Spare Tire a "Space Saver" yes X no 

Is Spare Tire Standard Equipment X yes no 

TEST FLUID DATA 

Test F1uid Type: Red Stoddard Solvent #2 Spec. Grav.: 0.764 

Kinematic Viscosity 0.96 Centistokes 

Spill Point Volume* ?n g gal (SPV) 

Test Volume 1R * gal (90 to 91% of SPV) 

Fuel System Capacity (data from Owner's Manual) 19-1/2 gal 
Details of fuel system Engine operated fuel pump, Fuel tank is located 
under trunk area with fill tube on left side behind rear wheel, 



Electric Fuel Pump Yes x No Fuel Injection Yes _X No 

Does electric fue! pump operate with ignition switch "on" and the engine 
not operating Yes x No 

VEHICLE RESOUND AND CRUSH 

0verall Length of Test Vehicle: Pre-Test - R 199.5 / L 199.7 inches 

Post-Test = R 176.8 / L 177.4 inches 
C ru sh - R 22.7 / L 22,3 

F0R FR0NTAL IMPACTS, distance from front of test vehicle to the barrier 
after impact = 6,6 inches 



r With entire fuel system filled from fuel tank through carburetor bowl . 

3-3 6525-V-17 



Table 7 
POST-IMPACT DATA - STANDARDS 219 AND 301 

DATA SHEET 

TYPE 0F TEST X Fronta1 (90°) Impact 

Oblique( °) Inpact on Left (Driver's) Side 

Right Side 

Lateral or Side Impact on Left (Driver's) Side 



Right Side 



Rear Impact 

DATE 0F TEST s/7s/7Q TIME i^n TEMP 78 ° F 

VEHICLE NHTSA NG. 308-17-458 VIN FH22G9G217130 

REQUIRED VEHICLE VEL0CITY RANGE 34.5 to 35.5 mph 

IMPACT VEL0CITY (traps within 5 feet of impact event) 35.04 



Trap No. 1 - 35.04 mph Trap No. 2 = Failed mph 

Distance from the vehic1e's front bumper to the barrier face entering 

the vehicle ve1ocity measurement device - 58 

exiting the vehide ve1ocity measurement device * 18 



VEHICLE STATIC CRUSH (for fronta1 and rear impacts only) 

Driver's Side = 22 * 3 in Passenger's Side = 22,7 in 
Average = 22 - 5 in 
Crush Details: 
Compartment intrusion 9.0 !r 

VEHICLE STATIC CRUSH (for side impacts only) 

Amount of Crush = - inches on - side 

Crush Details: 



VEHICLE REBOUND (from rigid barrier only) 

Driver's Side = - in Passenger's Side = - in 
Average = 6.6 in 

REMARKS 



3-4 



6525-Y-17 




Zero Point (0,0) 



FR0NT VIEW 

With the zero coordinate for the X-Y grid located at the lower right corner 
(passenger side) of the windshield, record the following positions: 

(1) The area that the "Protected Zone" template was penetrated more than 
.25 inches by a vehicle component other than one which is normally in 
contact with the windshield. 



NONE 



Coordinates 


X 


Y 



















(2) The area beneath the "Protected Zone" that the inner surface of the 
windshield was penetrated by a vehicle component. 



NONE 



Coordinates 


X 


Y 



















(3) Record any windshield retention clips or brackets used to insure that 
the windshield would not disengage from the body. 



Figure 5 WINDSHIELD Z0NE INTRUSION, FMVSS 219 - DATA SHEET 

3-5 6525-V-17 




48.5 



i 



Lower edge of protected zone 




64,5 



FR0NT VIEW 0F WINDSHIELD 

Provide all dimensions necessary to reproduce the protected zone 

Method of adhering styrofoam to the windshield: 

Construction adhesiye applied to windshield surface and to brake 
side of styrofoam, then clamped in place until dry. 



Figure 6 PROTECTED Z0NE 



3-6 



6525-Y-17 



Details of windshield mounting (method of retention, type of trim, etc.): 
Windshield is bonded in place and has a chrome trim piece around the 



perimeter o£ the window 





Windshield Periphery 




Right Side 


Pre-Test 


Post-Test 


Retention % 


80 


80 


100% 


Left Side 


80 


80 


100% 


TOTAL 


160 


160 


100% 



The standard requires that Post-Test be a minimum of 75 percent of the 
Pre-Test total periphery measurement for vehicle not equipped with occupant 
passive restraints and 50 percent for each side of the windshield for 
vehicles which are equipped with occupant passive restraints. 



AREA QF RETENTI0N FAILURE 

1" CHROME 




Indicate width of moulding 



NO CRACKS 



FR0NT VIEW 



Figure 7 SUMMARY 0F FMVSS 212 DATA 



3-7 



6525-V-17 



Table 8 
"FUEL SYSTEM INTEGRITY" POST-IMPACT TEST DATA 
FMVSS Ho. 301-75 



TEST VEHICLE NHTSA NO. 308-17-458 



Test Date 8/28/79 



Vehide Manufacture/Make/Mode1 1979 Chrysler LeBaron 



Test vehicle fuel tank f i 11 ed to 90-91% of capacity with Stoddard Solvent and 
with electric fuel pump operating (if it will operate without engine 
operation). Part 572 test dummies located at each front designated seating 
position. 



TEST YEHICLE IMPACT TYPE 

^_ Prontal (35 mph) 

Oblique (30 mph|-with- 



driver 



passenger side 



barrier face first contacting 



Rear Moving Barrier (35 mph) 
Lateral Moving Barrier (20 mph) 



FUEL SPILLAGE MEASUREMENT 






Actual 


Max. Allow. 


From impact until vehicle 
motion ceases 





1 oz 


For 5 nrin. period after 
vehicle motion ceases 





5 02 


For next 25 min. 





1 oz/1 min 



(t +5)+25 

m 

TEST VEHICLE STATIC ROLLOVER 

Test information will be added to the fo11owing static ro11over data sheets 

(1) Figure 8A - Ro11over data for 0° to 90° test phase 

(2) Figure 8B - Rol1over data for 90° to 180° test phase 

(3) Figure 8C - Ro11over data for 180° to 270° test phase 

(4) Figure 8D - Rollover data for 270° to 360° test phase 

S0LVENT SPILLAGE DETAILS 
NONE. 



3-8 



6S25-Y-17 



VEHICLE NHTSA ID NO. 308-17-458 



Table 8A 
FMVSS NO. 301-75 STATIC ROLLOVER DATA SHEET 



TEST PHASE 

















^*JT^^7^^^^ 


4 

J/mm li 


8 


t" 55 ^ 


Zw 




vl* 


A i i 








,-Hy' 




Fuel Filler 
Cap Location 



^T/NOTE: If side fill 



rotate to filler, 
cap is down. 




DETERMINATION 0F S0LVENT COLLECTION TIME PERIOD 

Rollover Fixture 90° Rotation Time = 
(Spec. Range - 1 to 3 min.) 

FMVSS 301-75 Position Hold Time 

TOTAL 

Next Whole Minute Interval = 

FMVSS 301-75 REQUIREMENTS 
Time Period 



2 


minutes 

minutes 
minutes 
minutes 


58 


seconds 


5 


00 


seconds 


7 


seconds 


8 







First 5 min. from onset of rotation 


6th min. 


7th min. 


8th min. if reqd. 


Maximum Allowable Solvent Spillage 










5 ounces 


1 ounce 


1 ounce 


1 ounce 


ACTU 


AL TEST VEHICLE S0LVENT SPILLAGE 










o 


n 









N0TE : Record spillage for whole minute intervals only as determined above 

S0LVENT SPILLAGE LOCATION(S) 
NONE. 



3-9 



6525-V-17 



VEHICLE NHTSA ID NO. 308-17-458 

Table 8B 
FMVSS NO. 301-75 STATIC ROLLOVER DATA SHEET 



TEST PHASE 



90 



180 




DETERMINATION 0F SQLVENT COLLECTION TIME PERIOO 

Rollover Fixture 90° Rotation Time = 2 minutes 
(Spec. Range = 1 to 3 min.) 

FMVSS 301-75 Position Hold Time = £ 

TOTAL = _L 

Next Whole Minute Interval = 8 

FMVSS 301-75 REOUIREMENTS 
Time Period 



57 seconds 



minutes 
minutes 
minutes 



m 



seconds 



57 seconds 



First 5 min. from onset of rotation 6th min. 



7th min 



8th min« if reqd. 



Maximum Allowable Solvent Spillage 



5 ounces 



1 ounce 



1 ounce 



1 ounce 



ACTUAL TEST VEHICLE SOLYENT SPILLAGE 



NOTE: Record spillage for whole minute intervals cnly as determined above 
SOLVENT SPILLAGE LOCATION(S) 



NONE 



3-10 



6525-Y-17 



YtrtlLLt NHIOH iU nu. ^-^ — "» 



Table 8C 
FMVSS NO. 301-75 STATIC R0LLQVER DATA SHEET 



TEST PHASE 






DETERMINATION 0F SOLVENT COLLECTION TIME PERIOO 

Ro11over Fixture 90° Rotation Time = 2 

(Spec. Range = 1 to 3 min.) 

FMVSS 301-75 Position Hold Time 

TOTAL 

Next Whole Minute Interval = 



minutes 



59 seconds 



5 minutes 00 seconds 

2 minutes 59 seconds 

8 minutes 



FMVSS 301-75 REQUIREMENTS 
Time Period 



i First 5 min. from onset of rotation 



5th min. \ 7th min. j 8th min. if reqd. j 



Maximum Allowable Solvent Spillage 



5 ounces 



1 ounce ! 1 ounce 



1 ounce 



ACTUAL TEST VEHICLE S0LVENT SPILLAGE 



NOTE : Record spillage for whole minute intervals only as determined above 

SOLYENT SPILLAGE LOCATION(S) 
NONE. 



3-11 



6525-V-17 



VEHICL£ NHTSA ID NO. 308-17-458 

Table 80 
FMVSS NO. 301-75 STATIC ROLLOVER DATA SHEET 



TEST PHASE 






DETERMINATION QF SOLVENT COLLECTION TIME PERIOD 

Rollover Fixture 90° Rotation Time = \ 

(Spec. Range = 1 to 3 min.) 

FMVSS 301-75 Position Hold Time = 5 



minutes 



59 seconds 



TOTAL 

Next Whole Minute Interval 

FMVSS 301-75 REOUIREMENTS 
Time Period 



5 minutes 

7 minutes 

3 minutes 



00 seconds 



59 seconds 



1 

! 
ACTU 


First 5 min. from onset of rotation 


6th min. 


7th min. 


! 8th 


min. if reqd. 


Maximum Allowable Solvent Spillage 










5 ounces 


1 ounce 


1 ounce 


i 
1 
t 


1 ounce i 


AL TEST VEHICLE S0LVENT SPILLAGE 





















l 

1 

i 


! 



NOTE : Record spillage for whole minute intervals only as determined above 

S0LVENT SPILLAGE LOCATION(S) 

NONE , __^_ 



3-12 



6525*-V-17 



APPENDIX A 
STILL PHOTOGRAPHS 



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APPENDIX B 
YEHICLE AND DUMMY RESPONSE DATA 



B-l 6525-V-17 



TEST NO. 308-17-458 
1979 CHRYSLER LeBARON 
VEHICLE DATA 

VEHICLE DATA FILTER CHANNEL CLASS 

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6525-V-17 



APPENDIX C 
DUMMY CERTIFICATION TESTS 



C-l 6525-V-17 



This test report contains results from certification tests performed 
on Alderson Research Laboratories Model ATD 30034, 50th percentile anthropomorphic 
test dummies, Serial Nos. 109, 814, which were completed on August 25, 1979. 
The results indicate that the dummies meet all of the performance requirements 
of the six standard tests as specified in 49 CFR Part 572, Federal Register, 
Vol. 42, No. 25, dated February 7, 1977. 

The tests were conducted at the Dummy Certification Test Facility 
of Calspan Corporation, Advanced Technology Center. A summary of the test 
results is presented in the following tables, Table 1C through 8C along with 
the Part 572 requirements. 



02 6525^V-17 



P.572 DUMMY CALIBRATION TEST DATA 



NHTSA DUMMY ID NO. 
LABORATORY TECHNICIAN 


109 
. "F"rĕd" Juliario 






APPROVE 


D BY: 






Pre-Test 
Calibration 


Post-Test 
Calibration 








. 




3/14/79-8/25/79 

67-74 
62-68 




Date ot uumtny LrdiiDrauiuu ----- 

Calibration Sequential Number for Dummy 

Temperature in Lab. (Spec. = 66 to 78°F) 

Relative Humidity in Lab. (Spec. = 10 to 70%) - 


TEST PARAMETER 


SPECIFICATION 






1. HEAD DROP TEST: 

a. Peak Resultant Accel. - 
b. Peak Lateral Accel. - - 
c. Time above 1006 


210 to 260G 


250 




<10G 


7 




0.9 to 1.5 ms 


1.0 




2. NECK BENDING TEST: 

a. Pendulum Speed - 

b. Pendulum Avg. Decel . 

(over t3 - t^) " 

c. Peak Resultant Head 

Acceleration 

d. Pendulum Decel . (t 2 -t«| ) 

e. Pendulum Decel . (t^-t^) 

f. Pendulum Decel. (t^-tj) 

g. Pendulum Direction 
Reversa1 Time - - - - 

h. Max. Head Rotation - - 

i. Chordal Displacement: 


21.5 to 25.5 fps 


22.12 




20 to 24G 


23 




26G maximum 


24 




<3 ms 


.75 




25 to 30 ms 


26 




<10 ms 


5 




>123 ms 


117 




63 to 73° 


63 












Head Rotation Angle - - 










0° 


Time 


-2 to 2 ms 







Displ . 


-.5 to .5 in 







30° 


Time 


25.6 to 34.4 ms 


29 




Displ . 


2.1 to 3.1 in. 


2.95 




60° 


Time 


40.3 to 51 .7 ms 


50 




Displ. 


4.3 to 5.3 in. 


5.25 




Maximum 

( •) 


Time 


53.2 to 66.8 ms 


58.8 




Displ . 


5.0 to 6.0 in. 


5,6 






Continued 


C-3 


6S2S- 1 


I/-17 



P. 572 DUWY CALIBRATION TEST DATA «... Continued 



NHTSA DUMMY ID MO. 109 











Pre-Test 
Calibration 


Post-Test 
Calibration 


TEST PARAMETER 


SPECIFICATI0N 


2. NECK BENDING TEST .... 
Continued 

i. Chordal Displacement; 

Head Rotation Angle — 










60° 


Time 


67.0 to 83.0 ms 


A7 




Displ. 


4.3 to 5.3 in. 


q . s 












30° 


Time 


85.4 to 104,6 ms 


95 




Displ. ' 


■2.1 to 3.1 in. 


?,.?, 


— , .. 




0* 


Time 101.0 to 123.0 ms 


116 






Displ . -.5 to 0.5 in. 


.15 




3. ABDOMINAL COMPRESSION 


< 
50 to 63 Ibs. 


56 




TE 

(P 
a. 


ST: 

reload = 10 pounds) 
Force @ 1" 


b. 


Force @ 1.3" 


73 to 88 Ibs. 


84 




4. LUMBAR FLEXION TEST: 

a. Force @ 20° 

b. Force @ 30° 

c. Force @ 40° 

d. Return Angle — - 


22 to 34 Ibs. 


26 




34 to 46 lbs. 


37,5 




46 to 58 Ibs. 


53 




12° maximum 


5 




5. CHEST IMPACT TESTS: 
a. High Speed 

(1) Probe Speed - - 

(2) Peak Delfection - 


21.78-22.22 fps 


21.85 




1 .7" maximum 


.8 






(3) Peak Resistive 
Force ------ 


2250 lbs. maximum 


1813 






(4) Internal 

Hysteresis 


50 to 70% 


60% 




b. 


Low Speed 

(1 ) Probe Speed 


13-86-14.14 fps 


14.03 




(2) Peak Def1ection - 


1.1" maximum 


.6 






(3) Peak Resistive 


1450 Ibs. maximum 


1243 






rui LC —————— 




(4) Internal 
Hysteres- 


is 


50 to 70% 


57% 





C-4 



6525-V~17 



P. 572 DUMMY CALIBRATION TEST DATA Continued 



NHTSA DUMMY ID NO. 109 





— 








Pre-Test 
Calibration 


Post-Test 
Calibration 




TEST PARAMETER 


SPECIFICATION 




6. KNEE IMPACT TESTS: 
a. Right Side — 

(1) Probe Speed 

(2) Maximum Porce - - 

(3) Time Above 1000# 


6.76 to 7.04 fps 


6,95 






1850 to 2500 Ibs 


2450 






1 .7 ms minimum 


2.2 






b. Left Side — 

(1) Probe Speed 

(2) Maximum Force - - 

(3) Time Above 1000# 


6.76 to 7.04 fps 


6,95 






1850 to 2500 Ibs. 


1850 






1.7 ms minimum 


2.1 







C-5 



6525-Y-17 



INSTRUMENT CALIBRATION INFORMATION 



NHTSA DUMMY ID NO. 109 



CALIB. SEQ. NOS. FOR DUMMY 



A. DUMMY INSTRUMENTS 



1. Head Accelerometers 



a. Triaxial unit 
b. Uniaxia1 units 



(1) Longitudinal (A^) 

(2) Lateral (A ) - - 

(3) Vertical (AJ - - 



Chest Accelerometers-- 
(Yehicle Crash Test Usage) 



a. Triaxial unit 
b* Uniaxial units 



(1 ) Longitudinal (A ) - 

(2) Lateral (A ) 

(3) Yertical (A z ) 



3. Chest Potentiometer 

4. Femur Load Cells — 
a. Right Side - - ■ 

b. Left Side 



MANUFACTURER 



SERIAL 
NUMBER 



B. CALIB . LAB . INSTRUMENTS : 

1. Pendulum Accelerometer - - 

2. Test Probe Accelerometer - 

3. Lumbar Flexion Test Push 



Force Gauge 



4. Abdominal Compression Test 
Force Gauge — - - - - - 



5. Abdominal Compression Test 
Displacement Gauge - 



ENDEYCO 



ENDEYCO 



ENDEYCO 



CEC 



ENDEYCO 



CEC 



HUMANOID 
SPECIAL 



GSE 



GSE 



CEC 



CEC 



BLH 



BLH 



CIC 



CF82/CS09 



CK54/CS41 



CE76/CY62 



22958 



CS75 



22705 



549 



548 



17547 



16928 



73141 



72952 



567-11 



DATE LAST" 
CALIBRATED 



DATE 0F 
NEXT 
CALIBRATION 



1/79 



1/79 



1/79 



1/80 



1/80 



1/80 



2/79 



1/79 



2/79 



1/80 



1/80 



1/80 



1/80 



1/79 



1/79 



2/79 



1/79 



1/80 



1/80 



1/80 



1/80 



C-6 



6525-Y-17 



P.572 DUMMY GALIbKAIlUN itsi uaia 



NHTSA DUMMY ID NO. 814 



LABORATORY TECHNICIAN: Fred Juliano 



APPR0VED BY: ^& K ^lJJ^/u^ 



Date of Dummy Calibration - - - - 

Calibration Sequential Number for Dummy 

Temperature in Lab. (Spec. = 66 to 78°F) 

Relative Humidity in Lab. (Spec. = 10 to 702) 



TEST PARAMETER 



1 . HEAD DROP TEST : 

a. Peak Resultant Accel 
b. Peak Lateral Accel . 
c. Time above 100G - - 



2. NECK BENDING TEST : 

a. Pendulum Speed - 

b. Pendulum Avg. Decel . 
(over t3 - t^) — " " 

c. Peak Resultant Head 
Acceleration - - - - 

d. Pendulum Decel . (t^-t^ ) 

e. Pendulum Decel . (tg-t^) 

f. Pendulum Decel . (t^-t^) 

g. Pendulum Direction 
Reversal Time - - - - 

h. Max. Head Rotation - - 

i. Chordal Displacement: 

Head Rotation Angle - - 



30' 



60' 



Maximum 

( °) 



Time 



Displ 



Time 



Displ 



Time 



Displ. 



Time 



Displ 



Continued 



SPECIFICATI0N 



210 to _260G 



<10G 



0.9 to 1.5 ms 



Pre-Test 
Calibration 



8/14/79-8/25/7« 
74 

60 



21.5 to 25.5 fps 



20 to 24G 



26G maximum 



<3 ms 
25 to 30 ms 



<10 ms 



>123 ms 



63 to 73 



-2 to 2 ms 



5 to .5 in 



25.6 to 34.4 ms 



2.1 to 3.1 in 



40.3 to 51 .7 ms 



4.3 to 5.3 in. 



53.2 to 66.8 ms 



5.0 to 6.0 in 



C-7 



230 



10 



1,0 



Post-Test 
Calibration 



21.64 



20 



22 



1.5 



25 



120 



68 



29 



2.65 



47 



4.80 



65 



5.40 



6525-V-17 



P. 572 DUMMY CALIBRATION TEST DATA Continued 



NHTSA DUMMY ID NO 



814 











Pre-Test 
Calibration 


Post-Test 
Calibration 


TEST PARAMETER 


SPECIFICATION 


2. NECK BENDING TEST .... 
Continued 

i. Chordal Displacement: 

Head Rotation Angle — 










60° 


Time 


67.0 to 83.0 ms 


80 




Displ. 


4.3 to 5.3 in. 


4.75 












30* 


Time 


85.4 to 104.5 ms 


100 




Displ. 


2.1 to 3.1 in. 


2.3 






0° 


~Time 


101.0 to 123.0 ms 


119 


i 




Displ. 


-.5 to 0.5 in. 


,1 


i 


3. AB 
TE 

(P 
a. 


DOMINAL COMPRESSION 
ST: 

reload = 10 pounds) 

fnvra (31" _____ 


50 to 53 Ibs. 


58 




rurcc l? 1 _____ 


b. Force 8 1.3" 


73 to 88 Ibs. 


86 




4. LUMBAR FLEXION TEST: 

a. Force <? 20° 

b. Force 1? 30° 

c. Force @ 40° 

d. Return Angle - - - 


22 to 34 Ibs. 


28 




34 to 46 Ibs. 


34,5 




46 to 58 Ibs. 


47 




12° maximum 


6° 




5. CHEST IMPACT TESTS: 
a. High Speed 

(1) Probe Speed - - 

(2) Peak Delfection - 


21.78-22.22 fps 


21 . 82 




1 .7" maximum 


1.1 






(3) Peak Resistive 

Pny*ro — ->-.-.-.-» 


2250 Ibs. maximum 


1916.6 






(4) Internal 

Hysteresis 




50 to 70% 


70 




b. 


Low Speed 

(1) Probe Speed 


13-86-14.14 fps 


13.88 




(2) Peak DeHection - 


1.1" maximum 


.95 






(3) Peak Resistive 

Frtv»^a -»-»-__-•__■ 


1450 Ibs. maximum 


1243,2 






rut ,c -»_--■_--»-» 




(4) Internal 
Hysteresi 


s 


50 to 70% 


68 





C-8 



6525-V-17 



L 



P.572 DUMMY CALIBRATION TEST DATA Continued : 



NHTSA DUMMY ID NO. 814 



TEST PARAMETER 



6. KNEE IMPACT TESTS : 
a. Right Side — 

(1) Probe Speed 

(2) Maximum Force - - 

(3) Time Above 10QO# 



Left Side - 

(1) Probe Speed - - ■ 

(2) Maximum Porce - • 

(3) Time Above 1000# 



SPECIFICATION 



6.76 to 7.04 fps 
1850 to 2500 Ibs 



1 .7 ms minimum 



6.76 to 7.04 fps 
1850 to 2500 Ibs. 



1.7 ms minimum 



Pre-Test 
Calibration 



6.96 



2075 



2.2 



7.01 



2200 



2.1 



Post-Test 
Calibration 



c-9 



6525-Y-17 



INSTRUMENT CALIBRATION INFORMATION 



NHTSA DUMMY ID NO. 814 



CALIB. SEQ, NOS. FOR DUMMY 



DUMMY INSTRUMENTS: 

1. Head Accelerometers 



a. Triaxial unit - - - - - 
b. Uniaxia1 units 

(1) Longitudinal (A ) - 

(2) Lateral (A ) 

(3) Vertical (A z ) 

2. Chest Accelerometers — 
(Vehicle Crash Test Usage) 

a. Triaxial unit - - - - - 

b. Uniaxial units 

(1) Longitudinal (A ) - 

(2) Lateral (A ) 

(3) Vertical (AJ 



3. Chest Potentiometer - - 

4. Femur Load Cells — 

a. Right Side 

b. Left Side 



B. CALIB . LAB . INSTRUMENTS : 

1. Pendulum Accelerometer - - 

2. Test Probe Accelerometer - 

3. Lumbar Flexion Test Push 
Force Gauge - - - 

4. Abdominal Compression Test 
Force Gauge ------- 

5. Abdominal Compression Test 
Displacement Gauge - - - - 



MANUFACTURER 


SERIAL 
NUMBER 


DATE LAST" 
ICALIBRATED 


| DATE 0F 
I NEXT 
JCALIBRATION 










ENDEVCO 


CF82/CP30 


1/79. 


1/80 


ENDEVm 


CK54/CE18 


1/79 


1/80 


ENDEVCO 


CF76/CL79 


1/70 


1/80 










CEC 


22595 


1/79 


1/80 


ENDEVCO 


CTOl 


1/79 


1/80 


CEC 


22703 




i/8o ; 


HUMANOID 
SPECIAL 






1/80 j 


D.V. 


1927 


1/79 


1/80 


D.V. 


1928 


1/79 


1/80 


CEC 


17547 


2/79 


1/80 


CEC 


16928 


1/79 


1/80 


BLH 


73141 




% 


BLH 


72952 






CIC 


567-11 






C-10 




6525-V-17 





Electronic Test Eguipment 

The complement of signal conditioning recording and display equip- 
ment used in conjunction with dummy certification testing is shown m 
Figure 8, 

• Data Acquisition - Sangamo Mod. 3500 14 channel FM Tape 
Transport (recording speed: 60 in/sec). 

• Data Reduction - Brush Mark 260 six channel recorder or 
Pace X-Y plotter. 

• Signal Conditioning - Calspan designed and fabricated bridge 
amplifiers providing gain, balance, and shunt calibration of 
all sensor inputs. 

t Computational Equipment - Calspan designed and fabricated 
analog computer consisting of operational amplifiers in 
circuit configurations providing continuous computation of 
acceleration vector magnitude and Severity Index relationships 

• Signal Filtering - Calspan designed and fabricated second 
order active filters (six channels) with selectable frequency 
responses consistent with SAE J211b Class 60, 180, 600 and 
1000 requirements. Filters are compensated for 32:1 real time 
expansion resulting from data recording at 60 in/sec and play- 
back at 1-7/8 in/sec. 

• Real Time Reference - Tektronix Time Mark Generator; 1 and 10 
millisecond is synchronously recorded with all certification 
data and reproduced at playback on all strip chart records. 

• The data acquisition, reproduction, and time reference equip- 
ment is maintained by Calspan's Equipment and Standards 
Laboratory (ESL), which is an NBS traceable calibration 
facility. Other special purpose equipment is maintained by 
qualified test facility personnel using support equipment 
maintained and standardized by all ESL. 



c _n 6525-Y-17 




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